Guidance for asteroid rendezvous
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[1] N. J. Niemi. INVESTIGATION OF A TERMINAL GUIDANCE SYSTEM FOR A SATELLITE RENDEZVOUS , 1963 .
[2] L. Cesari,et al. Asymptotic Behaviour and Stability Problems in Ordinary Differential Equations , 1960 .
[3] Robert A. Jacobson,et al. Use of Ballistic Arcs in Low Thrust Navigation , 1975 .
[4] M. Guelman. The closed-form solution of true proportional navigation , 1976, IEEE Transactions on Aerospace and Electronic Systems.
[5] W. E. Schmitendorf,et al. Stabilization via Dynamic Output Feedback: A Numerical Approach , 1991 .
[6] T. Carter,et al. Fuel-Optimal Rendezvous Near a Point in General Keplerian Orbit , 1987 .
[7] Lamberto Cesari,et al. Asymptotic Behavior and Stability Problems in Ordinary Differential Equations , 1963 .
[8] Robert A. Jacobson,et al. Terminal Navigation Analysis for the 1980 Comet Encke Slow Flyby Mission , 1973 .
[9] D. L. Jensen. Kinematics of rendezvous maneuvers , 1984 .
[10] James R. Wertz,et al. Spacecraft attitude determination and control , 1978 .
[11] Lincoln Wood,et al. Statistical analysis of trim maneuvers in low thrust interplanetary navigation , 1976 .
[12] C. L. Thornton,et al. Navigation capability for an ion drive rendezvous with Halley's Comet , 1978 .